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Jet Fuel Thermal Stability Investigations Using EllipsometryJet fuels are typically used for endothermic cooling in practical engines where their thermal stability is very important. In this work the thermal stability of Sasol IPK (a synthetic jet fuel) with varying levels of naphthalene has been studied on stainless steel substrates using spectroscopic ellipsometry in the temperature range 385-400 K. Ellipsometry is an optical technique that measures the changes in a light beam’s polarization and intensity after it reflects off of a thin film to determine the film’s thickness and optical properties. All of the tubes used were rated as thermally unstable by the color standard portion of the Jet Fuel Thermal Oxidation Test, and this was confirmed by the deposit thicknesses observed using ellipsometry. A new amorphous model on a stainless steel substrate was used to model the data and obtain the results. It was observed that, as would be expected, increasing the temperature of the tube increased the overall deposit amount for a constant concentration of naphthalene. The repeatability of these measurements was assessed using multiple trials of the same fuel at 385 K. Lastly, the effect of increasing the naphthalene concentration in the fuel at a constant temperature was found to increase the deposit thickness.In conclusion, ellipsometry was used to investigate the thermal stability of jet fuels on stainless steel substrate. The effects of increasing temperature and addition of naphthalene on stainless steel tubes with Sasol IPK fuel were investigated. It was found, as expected, that increasing temperature lead to an increase in deposit thickness. It wasAmerican Institute of Aeronautics and Astronautics6also found that increasing amounts of naphthalene increased the maximum deposit thickness. The repeatability of these measurements was investigated using multiple tests at the same conditions. The present work provides as a better quantitative tool compared to the widely used JFTOT technique. Future work will expand on the fuel types, temperature, and substrate materials.
Document ID
20170007697
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Nash, Leigh
(University of Central Florida Orlando, FL, United States)
Vasu, Subith S.
(University of Central Florida Orlando, FL, United States)
Klettlinger, Jennifer Lindsey
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 11, 2017
Publication Date
January 9, 2017
Subject Category
Propellants And Fuels
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN40522
Report Number: GRC-E-DAA-TN40522
Meeting Information
Meeting: SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX15AU28H
WBS: WBS 081876.02.03.04.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
thermal stability
ellipsometry
aviation fuel
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